algorithmic modeling for Rhino
I would like to implement a 4-digit airfoil formula as on the following page:
http://www.aerospaceweb.org/question/airfoils/q0041.shtml
Here I have my attempt to Step 2: mean camber line coordinates. But I'm obviously missing something.
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Impressive.Thanks for sharing.
Attached is the corrected definition.
Chris
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